Aerospace Engineering Dissertation Topics For Marvellous Dissertations

Date published July 31 2020 by Stella Carter

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Latest Aerospace Engineering Dissertation Topics for 2022-2023

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A systematic approach to design an Improved Turbofan Ramjet Engine for High Velocity Flights

Aims and Objective

To design an improved turbofan ramjet engine for sustained hypersonic flights.
To analyse the fuel consumption of the engine design and maximum thrust to weight ratio.
To analyse impact of varying altitude and weather on the performance of engine.
To evaluate the design and operational cost of the engine and their service life.

An Analytical study of AI Based Commercial Flights for Safe Air Travel

Aims and Objective

To analyse the benefits of integration of Artificial intelligence in commercial flights.
To evaluate the working of AI and its control over the aircraft.
To evaluate the provided effective outcomes of the program and its future impact on air travel.
The study will also provide the system for autonomous communication for AI based aircraft and their role in flight control.

Systematic analysis of Improved Aerodynamic Design for Efficient Fuel consumption During Long Flights

Aims and Objective

To design new and improved aero-dynamic design for commercial aircraft.
To evaluate the fuel consumption of new design.
To analyse the integration techniques to upgrade the existing aircraft design to new and improved models.
To evaluate the cost of maintenance of new design and its performance in unexpected conditions.

Analysing design of Advanced Computer Program For The maintenance and Operation Of Large-scale Satellite System

Aims and Objective

To design a new AI based computer program to guide the satellite in complex system.
To analyse the implementation techniques of new design in the existing satellite system.
To compare the effectiveness of new computer program verses existing programs.
To analyse the efficiency of the computer program and its maximum handling capacity.

Identifying design of Improved Composite material for aircraft to resist High Temperature during Supersonic flights.

Aims and Objective

To design the new and improved design for sustained supersonic flights.
To determine the maximum sheer, tensile and compressional stress of the material and its behavior in flying conditions.
To analyse the cost of material production and its maintenance cost.
To analyse the service life of the material and the ways to increase it.

A critical analysis of the novel hypervelocity terminal intercept guidance systems for deflecting and disrupting hazardous asteroids that potentially enters the stratosphere layer of Earth’s atmosphere.

Aim:

The aim of the study is to investigate the simulation of infrared and visual sensors and the computational modelling for developing a new system of hypervelocity terminal guidance of the small asteroids (50-150 in diameter). The research aims to develop the computation software techniques for the signal to noise ratio assessment of IR and visual sensors, assessment of maximum and minimum target detection ranges and the Graphic processing unit (GPU) accelerated simulations of the intercept guidance system on the basis of IR will also be developed. Additionally, the aim of the study is to use the model of scaled polyhedron for objects such as NASA’s OSIRIS Rex Bennu, Rosetta Comet mission 67P/C-G and the 433 Eros asteroid for the development of simulation tools that are GPU-based for the terminal guidance system which is IR based.

Objectives:

The objectives of the study are the following:

To develop the tracing algorithm of parallelized-ray for the simulation of accurate shadowing of the surface of the comets or asteroid which are of irregular shape.
To study and consider the approximation of polyhedron solid-angle.
To investigate the processing of the digital image by using the computational model for the determination of multiple or single effect location to estimate the practical feasibility of modern mission concept of planetary defence of using a multiple interceptor vehicle of kinetic energy or the intercept vehicle of hypervelocity asteroid.

A critical study on the modelling requirements for value formulation in the design of large scale complex engineered systems. A case study of NASA’s satellite network system.

Aim:

The aim of the study is to conduct a critical analysis of the requirement of modelling for the formulation of value in designing and developing engineering system which is large scale and complex. The research aims to study the satellite networking system of NASA. Therefore, the aim of the study is to assist the designers and developers in transitioning from the old necessities approach to the modelling of value. The research aims to use the design structure matrix which will be attribute-based to elaborate the procedure. Additionally, the research aims at quantifying the loss value because of the required usage. Furthermore, an extended study will be conducted on how the requirement presence has thereby resulted in the designs which are sub-optimal. Through this aim, the importance of using the approach of value over the approach of the requirement will be certainly justified. The overall requirement elimination process is not possible therefore, the study will develop an understanding of each of the requirements as not each requirement possess the same potential impact on the value. This aim will assist in areas like after the designing process completion, where the consumer wants to modify the requirements.

Objectives:

The objectives of the study are the following:

To assess the requirement impact on the sensitivity and value of these requirements on the finest design.
To analyze the value gap of to what extent there is a need to capture the uncertainty.
To study the usage of uncertainty’ probabilistic representation and its importance.

A novel evaluation of value-based model and analysis of autonomous unmanned aircraft systems based on the operational scenario.

Aim:

The aim of the study is to develop a model of value for the Unnamed Aircraft Systems (UAS) by taking into consideration the operational, environmental and technical scenarios involved for developing an analysis simulation of the decision in order to rate and analyze various UAS based on its readiness level of technology (TRL) and autonomy level (AL). Furthermore, this will assist in future to analyze the problem between the regulation to analyze the induced inefficiencies and the stakeholder preferences in the operation of UAS because of the requirement of policies. Therefore, the research aims to include utilizing a mixture of different frameworks and tools like decision analysis, Multidisciplinary Design Optimization and the Value-Driven Design to understand and analyze different factors which are involved while operating and designing UAS on a big scale for the use of civil applications and structural health monitoring.

Objectives:

The objective of the study will be:

To analyze how do the various operational and environmental scenario play a crucial role in the operation of UAS with respect to the task which is being performed.
To study how the class and physical characters of the UAS associated to the TRL and AL to the performance in the various operational scenario.
To evaluate whether the model of value-based can be used to conduct an analysis of risk on the UAS operation autonomously on the basis of societal, legal and ethical issues.

A critical analysis using game theory approach for negotiations in defence acquisitions in the context of value-driven design. A case study on USA’s aircraft system.

Aim:

The aim of the study is to analyze the new approaches usage in the defence acquisition’ negotiation phase, which will certainly form an important phase. Therefore, the study will analyze the required transition to the value by suggesting a performance-based price and value approach for defence acquisition. Therefore, the study aims to payoff maximization to both the contractor and the government establishing the governmental weapon system. The research will propose bargaining ideas from the game theory and will attempt to offer negotiation for the mathematical foundations.

Objectives:

The objectives of the study are the following:

To evaluate the effectiveness of game theory for improving the approach of value toward negotiation in performance-based and price based contracting scenario which certainly leads toward improved design system as compare to the one which is achieved through the old methods of driving requirement.
To determine the player order impact the bargaining game.
To determine whether a value-based approach joint with negotiation over other aspect be certainly utilized for bridging the gap between the defence acquisition setting contractor and the governmental preferences for the weapon system.

A novel approach methodology for rapid hypersonic flow predictions via surrogate modelling with machine learning and deep learning

Aim of the study
The aim of the study will be “To explore a novel approach methodology for rapid hypersonic flow predictions via surrogate modeling with machine learning and deep learning”.
Objectives of the study
The objectives of the study will be;

To explore the processes and modeling approaches involved in machine learning and deep learning.
To understand the concepts of surrogate-based modeling, optimization, and applications in engineering.
To review the approaches used for the rapid hypersonic flow predictions via surrogate modeling in the past years.
To compare the past and current approaches that can be used for the predictions of rapid hypersonic flow.
To develop a novel methodology for the rapid hypersonic flow predictions and to evaluate machine learning and deep learning.
To examine the aerodynamic data predictions for transonic flows via a machine learning-based surrogate model.
To evaluate the surrogate modeling approaches of aerodynamic simulations for multiple operating conditions using machine learning.
To examine the novel spatial-temporal prediction models for the unsteady wake flows based on a hybrid deep neural network.
To find out the significance of using the novel approaches for rapid hypersonic flow predictions via surrogate modeling with machine learning and deep learning.

A systematic review for understanding the effect of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform

Aim of the study
The aim of the study will be “To prepare a systematic review for understanding the effect of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform”.
Objectives of the study
The objectives of the study will be;

To understand the concept of the interactional aerodynamics and computational aeroacoustics.
To find out the impacts of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform.
To explore the design of aerodynamic optimization of proprotors for the convertible rotor.
To evaluate the optimization of the aerodynamic shape of a proporptor and its validation utilizing CFD and other experiments.
To examine the optimization of the aerodynamic shape of tiltrotor blades equipped with the continuous morphing aerofoils.
To find out the economic cost involved in the understanding of the effect of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform.
To do the critical review on analysing the impacts of interactional aerodynamics on computational aeroacoustics.
To assess the positive and negative effects of interactional aerodynamics on computational aeroacoustics.
To explore the strategies involved in understanding the impacts of interactional aerodynamics on computational aeroacoustics.
To compare the past and current approaches that can be employed to examine the impacts of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform.

A critical analysis of digital control law synthesis for Lockheed Martin’s innovative control effectors aircraft concept. Can this technology set the fundamentals for 6th generation fighter jets?

Aim of the study
The aim of the study will be “To do the critical analysis of digital control law synthesis for Lockheed Martin’s innovative control effectors aircraft concept. Can this technology set the fundamentals for 6th generation fighter jets?”

Objectives of the study
The objectives of the study will be;

To understand the concept of digital control law synthesis.
To understand the impacts of the technology for the 6^th generation fighter jets.
To explore the applications of digital control law synthesis for the 6th generation fighter jets.
To compare the technologies used in the past years with the applications of digital control law synthesis.
To set the scope and design requirements for the performance analysis to categorize the aircraft.
To examine the conventional and modern flight control system design process for the tailless aircraft Simulink model with innovative control effectors provided by Lockheed Martin
To evaluate open-loop dynamics revealed modal instabilities as well as state and control coupling.
To find out which method will achieve the stable augmented control of the innovative control effectors (ICE) aircraft throughout the flight envelope.
To understand the tailless fighter aircraft model for control-related research and development.

A critical study on the aerodynamic load identification and prediction of wind induced vibration on the outer structural and signal structures, in order to minimize them. A case study of Antonov 225.

Aims:
Several experiments have been performed on aerodynamic load models with defined parameters to evaluate the critical decreased dry- and ice-galloping velocity of a conductor at a given wind-related yaw angle of the conductor. However, the researcher observed that there is not a vast amount of research in the domain of mitigating the outer structural and signal structures by using aerodynamic load identification. Therefore, the researcher wants to fill this gap. The aim outlined by the researcher for carrying out this research is to study the aerodynamic load identification and prediction of wind induced vibration on the outer structural and signal structures, in order to minimize them. In this context, the researcher considers Antonov 225 aircraft so that research outcomes can be meet in an effective manner.
Objectives:
In order to endorse the primary objective of the research study, the researcher formulated the secondary objectives so that the potential outcomes of the study can be met in an effective manner. Following are the secondary objective of the study are as following:

To study the significance of aerodynamic load identification in Antonov 225 from theoretical perspective.
To critically analyze the aerodynamic load identification and prediction of wind induced vibration on the outer structural and signal structures.
To examine the impact of aerodynamic load identification for minimizing the wind induced vibration on the outer structural and signal structures.
To identify the potential factors affecting wind induced vibration on the outer structural and signal structures.
To investigate the implications of using aerodynamic load identification in Antonov 225 for diminishing the wind induced vibration on the outer structural and signal structures.

A novel experimental investigation on thermodynamic characteristics of dielectric barrier discharge (DBD) plasma and its applications for aircraft icing mitigation. A case study of Air bus A-380.

Aims:

In recent decades, the accretion of ice on aircraft or wind turbines has been generally recognised as a significant safety hazard. Therefore, the researcher wants to perform a research study in this domain. The purpose for conducting this research study is to perform an experimental investigation on thermodynamic characteristics of dielectric barrier discharge (DBD) plasma and its applications for aircraft icing mitigation. In this regard, the researcher takes specific note of the case of the Air Bus A-380 in order to support the main goal of the study being carried out.

Objectives:

The researcher designs the secondary objectives by narrowing down the primary objective into sub-parts in order to support the primary purpose of the study. Following are the secondary objectives:

To investigate the implications of dielectric barrier discharge (DBD) plasma from theoretical perspective.
To evaluate the approaches for icing control by using dielectric barrier discharge (DBD) plasma.
To perform an experimental study on Air Bus A-380 to bestow more reliable and safe solutions to mitigate aircraft icing.
To examine thermodynamic characteristics of dielectric barrier discharge (DBD) plasma and its applications for aircraft icing mitigation.
To provide relevant recommendations to effectively utilizing the thermodynamic features of dielectric barrier discharge (DBD) plasma for aircraft icing mitigation.

A critical study to reduce dimensionality of a commercial supersonic transport design space using active subspaces. A case study on using air freight to decreasing dependency on sea freight transport.

Aims:

The speed of commercial aircraft has been limited for decades by the sound barrier. However, recent noticeable increases in air travel and the acknowledgement of time as a desirable commodity for travelers have called for quicker, more efficient commercial transport. Therefore, the researcher wants to conduct the research study in the domain of aerospace by specifically considering supersonic transport design. The aim of researcher in this study is to perform a critical study on reducing the dimensionality of a commercial supersonic transport design space by using active subspaces. In this context, the researcher wants to make use of air freight to minimize reliance on sea freight transport.

Objectives:

The researcher has developed secondary objectives in order to support the main objectives of the research, which are as follows:

To comprehend the implications of using active subspaces for reducing dimensionality of a commercial supersonic transport design.
To critically analyze the impacts of using active subspaces air freight for decreasing dependency on sea freight transport.
To build a framework for commercial supersonic architecture that involves active subspace surrogates to enhance the exploration of design space.
To provide adequate recommendations on effectively using active subspaces air freight for reducing the dependency on sea freight transport.

A critical evaluation of supersonic boundary layers over an adiabatic wall with deformations. Can we expect return of supersonic passenger airliners in near future?

Aims:

The aim or carrying out this research study is to critically evaluate the supersonic boundary layers over an adiabatic wall with deformations. In this regard, the researcher wants to analyze the use of supersonic boundary layers for bringing back supersonic passenger airliners in future.

Objectives:

The primary of this research study is to evaluate the supersonic boundary layers over an adiabatic wall with deformations. Moreover, the researcher is inclined to explore the underlying factors which can guarantee the performance of the forthcoming supersonic passenger airliners. For the purpose of supporting the primary objectives of the research, the researcher formulated secondary objectives which are as following:

To investigate the implications of supersonic boundary layers over an adiabatic wall encompassing deformations.
To critically evaluate which aspects of supersonic boundary layers can be beneficial over an adiabatic wall to bring back supersonic passenger airliners in near future.
To explore which factors could guarantee the performance of the forthcoming supersonic passenger airliners.
To investigate prospective passengers' views of supersonic transport as a potential future mode of transportation.
To provide appropriate recommendations on successfully using supersonic boundary layers for bringing back supersonic passenger airliners in future.

A systematic study for exploring multi-objective aerodynamic design using multi-fidelity methods and novel pareto set identification techniques.

Aims:

For modern engineered systems like unmanned aerial systems and turbomachinery, the design of aerodynamic surfaces is essential. Therefore, the researcher wants to explore the multi-objective aerodynamic design by using different methods and techniques. In order to conduct this research study, the researcher has formulated the key aim, which is to perform a systematic study on exploring multi-objective aerodynamic design. The researcher is inclined to explore the multi-objective aerodynamic design using multi-fidelity methods and novel pareto set identification techniques.

Objectives:

The primary objective of this research is to fill the knowledge gap and explore alternatives for multi-objective aerodynamic architecture experimentation that are useful in multi-fidelity. In order to foster the primary objective of the research project, the secondary goal is designed by the researcher to enable the future findings of the study to be reached effectively. The secondary of the study are as following:

To study the concept of aerodynamic design from theoretical perspective.
To explore multi-objective aerodynamic design using multi-fidelity methods.
To investigate novel pareto set identification techniques that aligns with multi-objective aerodynamic design.
To assess the scalability of using the multi-fidelity methods and novel pareto set identification techniques.
To achieve optimized solutions which are non-commensurate using multi-fidelity techniques in the vicinity of a design configuration.

TYPE	SUBJECT
BS	An exploratory study using numerical investigations of bio inspired blade designs to reduce broadband noise in aircraft engines and wind turbines
BS	Elicitation and formal specification of run time assurance requirements for aerospace collision avoidance systems

Aerospace Engineering Dissertation Ideas For Staggering Dissertations

Aerospace engineering is a very vast and innovative field. Therefore, aerospace engineering dissertation ideas will prove to be more helpful for you which you can customize into your favourite topic, rather than a handful of aerospace engineering dissertation topics. For this reason our market specialist senior expert writers have also prepared a free list of the best aerospace engineering dissertation ideas that you can use to custom make aerospace engineering dissertation topics for yourselves.

1.0 A critical analysis of the lag parameter approach for turbulence modelling of the common and general air routes taken by passenger airlines in order to make them safer.

Aim:

The aim of the study is to conduct a critical analysis of the lag parameter method for the modelling of turbulence of general and common air route taken by airline passenger to make themselves safe. Therefore, the research aims to identify the factors of service quality in the airline industry.

Objectives:

The primary objective of the study is to achieve the aim of the study. However, the primary objective of the study can be achieved through various secondary objectives. Therefore, the secondary objectives of the study are:

To determine the procedures and methods that the airline must follow in order to offer safe and secure air travel.
To evaluate how the service quality of airline can be improved.
To evaluate the association between the profitability of airline and the service quality.

2.0 An experimental analytical investigation on wind turbine icing physics and anti- / de-icing technology. What is the most cost-efficient approach for aircraft flying at extremely high altitudes

Aim:

The aim of the study is to conduct an experimental analysis on the de-icing/anti-de-icing technology and the icing physics of wind turbine. The research aims to analyze which approach is cost-efficient for the aircraft who are flying at enormously high altitudes. Therefore, the research aims to explain the physics pertinent of icing toward wind turbines. Furthermore, the research aims to suggest robust and effective mitigation strategies of ice for the wind turbines.

Objectives:

The objectives of the study are the following:

To measure the process of active ice accretion over the blade surfaces of the wind turbine.
To analyze the ice accreting blades’ aerodynamic penalties.
To promote and encourage a fine understanding regarding the transfer of heat during the process of icing.
To suggest mitigation strategies of ice for the wind turbine blade.
To analyze the effectiveness, flexibility, central control and mass-production possibilities, economical efficiencies and safety of the proposed suggestions.
To evaluate which approach is cost-efficient for high altitude flying of aircraft.

3.0 A critical exploratory investigation on bio-inspired surface coatings for aircraft icing mitigation. Can nanotechnology be the permanent solution for surface icing problems?

Aim:

The aim of the study is to conduct a critical exploratory analysis to determine the bio-inspired surface coating for the icing mitigation of aircraft. The research aims to study that can the nanotechnology be the everlasting solution for the icing problem of the surface.

Objectives:

To develop a wind tunnel which will thereby quicken the droplets of water and determine the impact of highspeed droplet on the dynamics and coating of the bio-inspired surface.
To establish an accelerated and smooth spray generator to illustrate the bio-inspired surface durability.
To measure and quantify the details of the flow of the droplets which are wind-drive and to develop a theoretical model for forecasting the motion of wind-driven droplet on the different surface coating which are bio-inspired.
To offer a suggestion for the promising coating selection for icing mitigation of aircraft.

4.0 A novel dynamic analysis of composite wind turbine blade. How much stronger, sturdier and long-lasting are these composite blades when compared with the conventional ones?

Aim:

The aim of the study is to conduct a dynamic analysis of the complex wind turbine blade. The research aims to study the effectiveness of these composite blade. Furthermore, the aim of the study is to evaluate how much long-lasting, sturdier and stronger these blades areas compare to old ones. Therefore, the purpose of the study is to develop a basis for analyzing the level of accuracy required in the prediction model of load by comparing the wind turbine blade composite material results for the experimental wind loads set. Additionally, the research aims to evaluate how the wind forecasting dynamics can be enhanced for reliable, economical and safe operations of the wind turbines. The research will study the procedure of blade modelling, aerodynamic load calculations form the wind data collection and the analysis of fatigue for the wind turbine blade.

Objectives:

To study complex blades of wind turbines.
To evaluate the effectiveness of each blade.
To analyze as compare to conventional blades, how stronger these blades are?

5.0 A critical study on the management for electrical vertical take-off and landing (eVTOL) aircraft in on-demand urban air mobility.

Aim:

The aim of the study is to study the electrical vertical landing and takeoff (VTOL) aircraft management in urban air mobility which are on-demand. The study aims to develop the most energy effective arrival trajectory with battery endurance that is limited, eVTOL type and the particular CONOP (Concept of operation). The research aims to meet the allocated RTA constraint with secure eVTOL separation requirement of aircraft and partial vertiport time slot of arrival.

Objectives:

To study the scheduling of eVTOLs and the sequence of arrival.
To solve and formulate the scheduling problem and sequencing for assorted eVTOLs fleet in order to enable efficient and safe UAM operations.

6.0 How effective will this transport system be in providing medical assistance to individuals in overpopulated urban hub cities

Aim:

The aim of the study is to evaluate the effectiveness of the airline system in offering medical help to people in the urban hub cities which are overpopulated. Therefore, the research emphasizes on the urban development central aspect that is urban form and transport and studies how these two will certainly shape the provision of goods and services, access to people and the information in cities.

Objective:

To evaluate the effectiveness of airline in offering medical support.
To investigate the association between passenger loyalty, passenger satisfaction and the service quality of the airline.
To determine factors which contribute to the service quality of airlines.

7.0 A study on the technological development requirements for assessment in making space habitat possible.

Aim:

The aim of the study is to understand the requirement of technological development for the assessment and valuation in the space habitat making. Therefore, the study aims to fill the current gaps in technology selection and subsystem sizing. The aim of the study is to develop a methodology to size dynamically subsystems of space habitats and choose technologies to carry various missions.

Objectives:

To evaluate the requirement of technological advancement for the development of space habitats.
To analyze how the subsystem can be size dynamically and chose for various missions.
To evaluate the challenges of space exploration.
To analyze the space habitats characteristics.

8.0 A critical exploration and performance analysis of novel techniques for optimising supersonic descent staging aerodynamic. How will this technology help in manned landing on Mars’ surface?

Aim:

The aim of the study is to conduct a critical exploration and the analysis of the performance of the techniques for the optimization of supersonic descent production aerodynamics. The study aims to analyze how this technique will certainly support and assist in manned landing on the surface of Mars.

Objectives:

To evaluate the performance of the novel techniques in the optimization of supersonic descent production aerodynamics.
To analyze the effectiveness of these techniques.
To study how these technologies will certainly help in manned landing on the surface of Mars.

9.0 A novel approach of implementing deep learning algorithms for improving the spacecraft’s attitude and orbit control system (AOCS).

Aim:

The aim of the study is to conduct a novel approach on how the algorithms of deep learning can be implemented for enhancing the attitude of spacecraft and orbit control system (AOCS).

Objectives:

To explore the deep learning application on the isolation and fault detection in the AOCS.
To establish a framework for additional research for the aerospace deep learning.
To create or acquire the important telemetry that is to be used for testing and training the classifiers of AOCS.
To develop a model of simulation which is certainly capable of the simulation of on-orbit faults.
To analyze the basis of spacecraft attitude control and determination.

10. A critical evaluation of using large eddy simulation (LES) and machine learning augmentation for flow over bumps enabled turbulence modelling in space crafts.

Aims and objectives

Aims

The aim of this study is that to critically evaluate the using of large eddy simulation and the machine learning augmentation for flow over bumps enabled turbulence modelling in the space crafts. However, large eddy simulation is the mathematical model which used the computational fluid dynamics for turbulence. The turbulent flow with two-dimensional bumps by the well resolved large eddy simulation. The data augmentation also reduces overfitting when training a machine learning. This is also closely related to the oversampling in data analysis. The optimization method is used to extract fields of variables used in the turbulence closure models.

Objectives

The objectives of this study are the following:

To critically analyse the large eddy simulation LES and data augmentation.
To analyse the turbulence modelling in space crafts.
To evaluate the large eddy simulation and machine learning augmentation for flow over bumps enabled turbulence modelling in space crafts.

11. A novel approach of using hybrid electric distributed propulsion for vertical take-off and landing spacecraft. How effective will this system be for entering and leaving atmospheres of different planets?

Aims
The aim of this study is that it is the novel approach use of the hybrid electric distributed propulsion for landing and vertical take-off of the space crafts. This is the study also analyse the effectiveness of this system for the atmosphere in entering and leaving in different planets. This research also explores the interaction between the hybrid electric power system (HEPS) and aerodynamics and control for vertical take-off and landing (VTOL) aircraft applications with the selection of the configuration for evaluation of interaction with the hybrid power system.
Objectives
The objectives of this study are the following:

To analyse the Hybrid electric power system (HEPS) and vertical take-off and landing (VTOL).
To assess the novel approach or idea of using hybrid electric distributed propulsion for vertical takeoff and landing spacecraft.
To assess the system's affectivity for entering and leaving the atmosphere of different planets.
To analyse the impact of hybrid electric distributed propulsion for vertical take-off and landing spacecraft and atmosphere on other planets.

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Q1 How can I make my aerospace engineering dissertation topics more attractive?

A few pointer to make your dissertation topics more attractive are that you should make them compelling by using flashy and witty words that instantly capture a reader’s attention. You should also make your topics a bit informative to reveal the central idea behind your dissertation and lastly you should also make them indicative.

Q2 What are some Do’s of writing a dissertation?

Your dissertation’s tone should be formal but yet creative. Your dissertation should be properly structured into chapters and sub chapters. You should be careful about plagiarism, try to keep it as low as possible and lastly hire a professional editor once you are done with your dissertation.

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Q4 What is the word count of a dissertation?

The wordcount for your dissertation depends on a number of things e.g. your level of degree, your topics, the type of research involved. And the word count ranges from anywhere in between 10000 to 80000 words.

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Aerospace Engineering Dissertation Topics For Marvellous Dissertations

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Latest Aerospace Engineering Dissertation Topics for 2022-2023

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Aerospace Engineering Dissertation Ideas For Staggering Dissertations

Aims and objectives

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